摘要
针对某型导弹制导控制系统质心控制回路,提出了标称弹道方法。这种方法有以下特点:充分利用惯性导航系统提供的导弹的速度、位置及姿态信息,经过控制计算机形成控制指令;原理简单、容易执行。通过数字仿真表明了标称弹道方法完全能满足指标要求,是可行的。
Aiming at the control loop of the missile＇s guidance and control system, the schema trajectory is presented. This method has several features as follows： using missile＇s information such as velocity, position and attitude angle provided by navigation system, control computer produce control order. It has simple principle and could be realizable. The result of the simulation shows that this method meets the demands and is effective.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第3期38-39,45,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
复合制导
标称弹道
比例导引
导弹
composite guidance
schema trajectory
proportional guidance
